# N911VU: 2005 Pilatus PC-12/45

- Status: Valid registration
- Airframe: [Pilatus PC-12/45](https://openairdocs.org/model/pilatus-pc-12-45) (registry code 7090051, 12 seats)
- Engine: [Pratt & Whitney Canada PT6A-67B](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67b) (registry code 52158)
- Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) (Pilatus Aircraft Ltd.), [TCDS E26NE](https://openairdocs.org/tcds/E26NE) (Pratt & Whitney Canada Corp.) (OpenAirDocs)
- Serial number: 639
- Year built: 2005
- Type: Fixed wing single engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: June 28, 2005
- Certificate issued: February 24, 2015
- Expires: February 29, 2028
- Mode S code: AC9C50
- Registered owner: [Air Methods LLC](https://openairdocs.org/faa-owner/AIR%20METHODS%20LLC)
- Location: [Greenwood Village, CO](https://openairdocs.org/faa-place/CO/Greenwood%20Village)
- Owner type: LLC
- Owner's area on the map: 39.6120° N, 104.8828° W: Placed by OpenAirDocs at the center of ZIP code 80111, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=911VU
- Page: https://openairdocs.org/aircraft/N911VU

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 52 in force

### Matched by airframe (Pilatus PC-12/45)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2024-08-07](https://openairdocs.org/ad/2024-08-07): Main Landing Gear Attach Section · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jun 3, 2024
- [AD 2023-09-12](https://openairdocs.org/ad/2023-09-12): Air Conditioning System Wiring · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jul 5, 2023
- [AD 2021-24-01](https://openairdocs.org/ad/2021-24-01): Aerodynamic Faring · Pilatus PC-12/45, PC-12/47 and PC-12/47E with STC SA00634DE. Effective Jan 13, 2022
- [AD 2020-21-23](https://openairdocs.org/ad/2020-21-23): Stabilizers · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Dec 7, 2020
- [AD 2016-18-05](https://openairdocs.org/ad/2016-18-05): Power Plant · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Oct 6, 2016
- [AD 2016-12-01](https://openairdocs.org/ad/2016-12-01): Wings · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Jul 15, 2016
- [AD 2015-19-15](https://openairdocs.org/ad/2015-19-15): Flight Controls · Pilatus PC-12, PC-12/45 and PC-12/47E. Effective Nov 3, 2015
- [AD 2008-07-11 R1](https://openairdocs.org/ad/2008-07-11-R1): Flight Controls · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Mar 25, 2013
- [AD 2009-08-11](https://openairdocs.org/ad/2009-08-11): Ice and Rain Protection · Pilatus PC-12 and PC-12/45. Effective May 26, 2009
- [AD 2009-05-07](https://openairdocs.org/ad/2009-05-07): Rear stick-pusher cable · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Mar 30, 2009
- [AD 2008-07-11](https://openairdocs.org/ad/2008-07-11): Pitch trim actuator · Pilatus PC-12, PC-12/45 and PC-12/47. Effective May 9, 2008
- [AD 2008-02-03](https://openairdocs.org/ad/2008-02-03): MLG special bolts · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Feb 20, 2008
- [AD 2007-21-11](https://openairdocs.org/ad/2007-21-11): Oil pile assemblies · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Nov 5, 2007
- [AD 2007-03-06](https://openairdocs.org/ad/2007-03-06): Executive seats equipped with pedestal legs · Pilatus PC-12 and PC-12/45. Effective Mar 8, 2007
- [AD 2006-16-13](https://openairdocs.org/ad/2006-16-13): Lug fittings. · Pilatus PC-12 and PC-12/45. Effective Sep 18, 2006
- [AD 2006-08-11](https://openairdocs.org/ad/2006-08-11): Crew seat bucket assemblies · Pilatus PC-12 and PC-12/45. Effective Jun 2, 2006
- [AD 2005-22-13](https://openairdocs.org/ad/2005-22-13): Left and right main landing gear (MLG) assemblies · Pilatus PC-12 and PC-12/45. Effective Dec 19, 2005
- [AD 2005-22-04](https://openairdocs.org/ad/2005-22-04): Nose landing gear (NLG), main landing gear (MLG), and MLG shock absorber  
 assemblies · Pilatus PC-12 and PC-12/45. Effective Dec 12, 2005
- [AD 2005-11-06](https://openairdocs.org/ad/2005-11-06): Pitch actuator · Pilatus PC-12 and PC-12/45. Effective Jul 18, 2005
- [AD 2005-04-16](https://openairdocs.org/ad/2005-04-16): Windshield de-ice wiring system · Pilatus PC-12 and PC-12/45. Effective Mar 8, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2005-01-11](https://openairdocs.org/ad/2005-01-11): Main Landing Gear (MLG) Actuator · Pilatus PC-12 and PC-12/45. Effective Feb 22, 2005
- [AD 2004-12-11](https://openairdocs.org/ad/2004-12-11): Outboard flap flexshafts · Pilatus PC-12 and PC-12/45. Effective Jul 26, 2004
- [AD 2004-06-05](https://openairdocs.org/ad/2004-06-05): Main landing gear shock absorber · Pilatus PC-12 and PC-12/45. Effective May 6, 2004
- [AD 2004-04-01](https://openairdocs.org/ad/2004-04-01): Engine-driven pump housing · Pilatus PC-12, PC-12/45 and PC-7. Effective Mar 29, 2004
- [AD 2003-20-15](https://openairdocs.org/ad/2003-20-15): Fuel booster pump · Pilatus PC-12 and PC-12/45. Effective Oct 10, 2003
- [AD 2003-11-17](https://openairdocs.org/ad/2003-11-17): Pressure dome · Pilatus PC-12 and PC-12/45. Effective Jul 28, 2003
- [AD 2003-09-11](https://openairdocs.org/ad/2003-09-11): Pedestal Leg Assembly on Aft Facing Passenger Seats · Pilatus PC-12 and PC-12/45. Effective Jun 16, 2003
- [AD 2003-07-10](https://openairdocs.org/ad/2003-07-10): Push switch caps · Pilatus PC-12 and PC-12/45. Effective May 12, 2003
- [AD 2002-14-22](https://openairdocs.org/ad/2002-14-22): Main Landing Gear (MLG) Assembly Bolts · Pilatus PC-12 and PC-12/45. Effective Aug 29, 2002
- [AD 2002-06-10](https://openairdocs.org/ad/2002-06-10): Connector and Oxygen Tubing and Related Components in Rear Seat Bench · Pilatus PC-12 and PC-12/45. Effective May 6, 2002
- [AD 2001-25-10](https://openairdocs.org/ad/2001-25-10): Flap Control System · Pilatus PC-12 and PC-12/45. Effective Jan 25, 2002
- [AD 2001-22-15](https://openairdocs.org/ad/2001-22-15): Cargo Doors · Pilatus PC-12 and PC-12/45. Effective Dec 26, 2001
- [AD 2001-11-02](https://openairdocs.org/ad/2001-11-02): Generator · Pilatus PC-12 and PC-12/45. Effective Jul 23, 2001
- [AD 2000-26-17](https://openairdocs.org/ad/2000-26-17): Windshield Deicing System · Pilatus PC-12 and PC-12/45. Effective Feb 24, 2001
- [AD 2000-11-14](https://openairdocs.org/ad/2000-11-14): Airframe Pneumatic Deicing Boots · Pilatus PC-12 and PC-12/45. Effective Jul 17, 2000
- [AD 2000-02-31](https://openairdocs.org/ad/2000-02-31): Stick Pusher System · Pilatus PC-12 and PC-12/45. Effective Mar 27, 2000
- [AD 99-24-09](https://openairdocs.org/ad/99-24-09): Flap Inboard Attachment Fittings · Pilatus PC-12 and PC-12/45. Effective Jan 14, 2000
- [AD 99-17-01](https://openairdocs.org/ad/99-17-01): Flap Drive Shafts · Pilatus PC-12 and PC-12/45. Effective Oct 1, 1999
- [AD 99-14-03](https://openairdocs.org/ad/99-14-03): Generator Cables · Pilatus PC-12 and PC-12/45. Effective Aug 17, 1999
- [AD 99-06-17](https://openairdocs.org/ad/99-06-17): Second Generator Control Unit · Pilatus PC-12 and PC-12/45. Effective Jun 16, 1999
- [AD 99-06-05](https://openairdocs.org/ad/99-06-05): Alternate Flap System · Pilatus PC-12 and PC-12/45. Effective Apr 16, 1999
- [AD 98-21-27](https://openairdocs.org/ad/98-21-27): Passenger Seats And Seat Rail Covers · Pilatus PC-12 and PC-12/45. Effective Nov 26, 1998
- [AD 98-20-28](https://openairdocs.org/ad/98-20-28): Airplane Flight Manual (AFM) - Limitations Icing · Pilatus PC-12 and PC-12/45. Effective Nov 4, 1998
- [AD 98-11-01 R2](https://openairdocs.org/ad/98-11-01-R2): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Sep 22, 1998
- [AD 98-11-20](https://openairdocs.org/ad/98-11-20): Lavatory Wall and Passenger Seat Configuration · Pilatus PC-12 and PC-12/45. Effective Jul 13, 1998
- [AD 98-08-26](https://openairdocs.org/ad/98-08-26): Fuel Tank Underwing Access Panels · Pilatus PC-12 and PC-12/45. Effective May 29, 1998
- [AD 98-07-18](https://openairdocs.org/ad/98-07-18): Propeller De-icing Controller · Pilatus PC-12 and PC-12/45. Effective Apr 28, 1998
- [AD 98-04-16](https://openairdocs.org/ad/98-04-16): Aileron Tie-Rod Jam Nuts · Pilatus PC-12 and PC-12/45. Effective Apr 2, 1998

### Matched by engine (Pratt & Whitney Canada PT6A-67B)

- [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024
- [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997

### Historical (superseded or no longer in force)

- [AD 2023-12-17](https://openairdocs.org/ad/2023-12-17) (historical): Horizontal Stabilizer, Spar/Rib · Pilatus PC-12, PC-12/47, PC-12/45 and 1 more. Effective Aug 7, 2023
- [AD 2022-19-03](https://openairdocs.org/ad/2022-19-03) (historical): Rudder Actuator, Main Landing Gear, Main Landing Gear Attach Section · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Oct 27, 2022
- [AD 2016-26-08](https://openairdocs.org/ad/2016-26-08) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Feb 9, 2017
- [AD 2014-22-01](https://openairdocs.org/ad/2014-22-01) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Dec 18, 2014
- [AD 2012-26-16](https://openairdocs.org/ad/2012-26-16) (historical): Time Limits · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Mar 26, 2013
- [AD 2009-14-13](https://openairdocs.org/ad/2009-14-13) (historical): Landing gear · Pilatus PC-12, PC-12/45, PC-12/47 and 1 more. Effective Aug 19, 2009
- [AD 2008-06-17](https://openairdocs.org/ad/2008-06-17) (historical): Rear stick-pusher · Pilatus PC-12, PC-12/45 and PC-12/47. Effective Apr 2, 2008
- [AD 2003-14-07](https://openairdocs.org/ad/2003-14-07) (historical): Nose landing gear (NLG) · Pilatus PC-12 and PC-12/45. Effective Sep 5, 2003
- [AD 2002-01-09](https://openairdocs.org/ad/2002-01-09) (historical): Gasket Material and Relief Valve Attachment Screws · Pilatus PC-12, PC-12/45 and PC-7. Effective Feb 28, 2002
- [AD 2000-21-14](https://openairdocs.org/ad/2000-21-14) (historical): Torque Oil-pressure Tubes and Py Pressure Pipe · Pilatus PC-12 and PC-12/45. Effective Dec 15, 2000
- [AD 99-19-32](https://openairdocs.org/ad/99-19-32) (historical): Actuator Internal Gear Systems · Pilatus PC-12 and PC-12/45. Effective Nov 8, 1999
- [AD 99-17-08](https://openairdocs.org/ad/99-17-08) (historical): Generator · Pilatus PC-12 and PC-12/45. Effective Oct 4, 1999
- [AD 98-11-01 R1](https://openairdocs.org/ad/98-11-01-R1) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Sep 22, 1998
- [AD 98-11-01](https://openairdocs.org/ad/98-11-01) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Jun 7, 1998
- [AD 97-23-04](https://openairdocs.org/ad/97-23-04) (historical): Fuel Tank Vent Valves · Pilatus PC-12 and PC-12/45. Effective Dec 1, 1997

## Information bulletins (advisory) (10 in force)

- [SAIB CE-17-13](https://openairdocs.org/saib/CE-17-13): Engine Oil Pressure; Torque Transducer Oil Pressure Pipe P-Clamp Installation. Issued May 19, 2017
- [SAIB CE-05-08](https://openairdocs.org/saib/CE-05-08): . Issued Oct 25, 2004
- [SAIB CE-04-70](https://openairdocs.org/saib/CE-04-70): . Issued Jul 8, 2004
- [SAIB CE-04-62](https://openairdocs.org/saib/CE-04-62): . Issued Apr 12, 2004
- [SAIB CE-04-60](https://openairdocs.org/saib/CE-04-60): . Issued Mar 30, 2004
- [SAIB CE-04-52](https://openairdocs.org/saib/CE-04-52): . Issued Feb 13, 2004
- [SAIB CE-03-19](https://openairdocs.org/saib/CE-03-19): . Issued Jan 22, 2003
- [SAIB CE-02-15](https://openairdocs.org/saib/CE-02-15): . Issued Feb 13, 2002
- [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015
- [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003

## NTSB investigations

None matched to N911VU.

## FAA accident and incident reports

None matched to N911VU.

## Service difficulty reports (1)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR QMLA2023092020073](https://openairdocs.org/sdr/QMLA2023092020073), Sep 18, 2023: EADI. FAILED. PILOT COMPLETED A NORMAL LANDING AT KLZU . WHILE TAXIING IN THE VICINITY OF TAXIWAY JULIET, PILOT AND THE MEDICAL CREW NOTED A STRONG, ELECTRICAL BURNING SMELL 

## Service difficulty reports on N911VU not matched to an aircraft (42)

They name N911VU, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR R7MR34116](https://openairdocs.org/sdr/R7MR34116), Apr 11, 2001: BEARING. DAMAGED. TURBINE, ANNULAR BALL BEARING, EXCESSIVE PITTING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR R7MR33270](https://openairdocs.org/sdr/R7MR33270), Feb 14, 2001: ANTENNA. INOPERATIVE. KA 92 ANTENNA, UNIT INOPERATIVE. GPS WILL NOT PICK UP SATELITE LINK. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR R7MR33448](https://openairdocs.org/sdr/R7MR33448), Jan 19, 2001: TRANSMITTER. INOPERATIVE. UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR R7MR33447](https://openairdocs.org/sdr/R7MR33447), Jan 19, 2001: TRANSMITTER. INOPERATIVE. UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR R7MA714132490](https://openairdocs.org/sdr/R7MA714132490), Sep 19, 2000: TRANSMITTER. INOPERATIVE. PRESSURE TRANSMITTER INOPERATIVE. TRANSMISSION GAUGE INDICATES (0). REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR R7MR33324](https://openairdocs.org/sdr/R7MR33324), Sep 16, 2000: PICKUP. INOPERATIVE. UNIT INOPERATIVE. ERRATIC NEEDLE ON N GAUGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 20001018SH014](https://openairdocs.org/sdr/20001018SH014), Jul 26, 2000: TRANSMITTER. FLUCTUATES. PRESSURE TRANSMITTER UNIT CAUSED PRESSURE GAUGE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
- [SDR 20000919SH014](https://openairdocs.org/sdr/20000919SH014), Mar 29, 2000: PICKUP. ERRATIC. NGP SPEED ERRATIC. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
- [SDR 20000621SH002](https://openairdocs.org/sdr/20000621SH002), Feb 23, 2000: MANIFOLD. DEFECTIVE. IMPROPER NOZZLE SPRAY PATTERN. REQUIRED 6000-HOUR INSPECTION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
- [SDR 20000918SH031](https://openairdocs.org/sdr/20000918SH031), Jan 27, 2000: PICKUP. INOPERATIVE. UNIT INOPERATIVE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. (X)
- [SDR 2000ZZZX784](https://openairdocs.org/sdr/2000ZZZX784), Dec 23, 1999: ANTENNA. INOPERATIVE. ANTENNA INOPERATIVE. WILL NOT LOCK-ON SATELLITE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX3799](https://openairdocs.org/sdr/99ZZZX3799), Jul 18, 1999: MANIFOLD. FAILED. MANIFOLD FAILED SB 0124. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX3881](https://openairdocs.org/sdr/99ZZZX3881), Jun 21, 1999: BEARING. WORN. BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX3882](https://openairdocs.org/sdr/99ZZZX3882), May 7, 1999: GUIDE. WORN. GUIDE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX3880](https://openairdocs.org/sdr/99ZZZX3880), May 7, 1999: GUIDE. WORN. GUIDE WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 99ZZZX1797](https://openairdocs.org/sdr/99ZZZX1797), Oct 5, 1998: SEAL. WORN. SEAL WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 98ZZZX1806](https://openairdocs.org/sdr/98ZZZX1806), Jan 14, 1998: BEARING. WORN. BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS, CORRECTED PROBLEM.
- [SDR 98ZZZX1807](https://openairdocs.org/sdr/98ZZZX1807), Dec 29, 1997: TRANSMITTER. ERRATIC. ERRATIC NR 1 TRANSMISSION OIL PRESSURE INDICATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 97ZZZX5074](https://openairdocs.org/sdr/97ZZZX5074), Sep 6, 1997: RESISTOR. FAILED. VARIABLE RESISTOR CAUSES CIRCUIT BREAKERS TO TRIP. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 97ZZZX5073](https://openairdocs.org/sdr/97ZZZX5073), Jul 17, 1997: TRANSMITTER. FAILED. TRANSMITTER UNIT CAUSES OIL PRESSURE GAUGE NEEDLE TO FLUCTUATE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 97ZZZX4132](https://openairdocs.org/sdr/97ZZZX4132), Mar 25, 1997: BLADE. DEFECTIVE. M/R BLADE FAILED BLADE INSPECTION PROGRAM. EXCESSIVE BULGING. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 97ZZZX2159](https://openairdocs.org/sdr/97ZZZX2159), Feb 21, 1997: TRANSDUCER. FAILED. TORQUE PRESSURE TRANSDUCER FAILED. NEEDLE SPINS ON GAUGE. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 96ZZZX3600](https://openairdocs.org/sdr/96ZZZX3600), Dec 28, 1995: LIGHT. CRACKED. TAIL LIGHT CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 96ZZZX3599](https://openairdocs.org/sdr/96ZZZX3599), Dec 8, 1995: LIGHT. CRACKED. TAIL LIGHT CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 96ZZZX3598](https://openairdocs.org/sdr/96ZZZX3598), Oct 26, 1995: LIGHT. CRACKED. TAIL LIGHT CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 96ZZZX532](https://openairdocs.org/sdr/96ZZZX532), Sep 8, 1995: SEAL. LEAKING. SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. ENGINE TOTAL CYCLES, 4,870.4.
- [SDR 96ZZZX531](https://openairdocs.org/sdr/96ZZZX531), Sep 8, 1995: SEAL. LEAKING. SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. ENGINE TOTAL CYCLES, 4,870.4.
- [SDR 96ZZZX1499](https://openairdocs.org/sdr/96ZZZX1499), Sep 8, 1995: TORQUEMETER. SHAFT. TORQUEMETER SHAFT RECEIVED IN DEFECTIVE CONDITION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 96ZZZX1685](https://openairdocs.org/sdr/96ZZZX1685), Jun 9, 1995: LIGHT. DEFECTIVE. LIGHT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
- [SDR 95ZZZY0994](https://openairdocs.org/sdr/95ZZZY0994), May 10, 1995: LIGHT. INOPERATIVE. LIGHT UNIT INOPERATIVE. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.
- [SDR 95ZZZY0993](https://openairdocs.org/sdr/95ZZZY0993), May 10, 1995: ROD END ASSY. WORN. ROD END ASSY WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.
- [SDR 95ZZZY0955](https://openairdocs.org/sdr/95ZZZY0955), May 10, 1995: BEARING. WORN. BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.
- [SDR 95ZZZX5585](https://openairdocs.org/sdr/95ZZZX5585), May 9, 1995: BEARING. WORN. BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 2 EACH NEW UNITS) CORRECTED PROBLEM.
- [SDR 95ZZZX2587](https://openairdocs.org/sdr/95ZZZX2587), Apr 17, 1995: INDICATOR. FLUCTUATES. NR 1 SUPPLY TANK NEEDLE FLUCTUATES ERRATICALLY. REPLACED WITH NEW UNIT. CORRECTED PROBLEM.
- [SDR 95ZZZY0725](https://openairdocs.org/sdr/95ZZZY0725), Apr 5, 1995: TRANSDUCER. DEFECTIVE. #2 OIL PRESSURE GAUGE FLUCTUATES. REPLACED WITH NEW UNIT CORRECTED PROBLEM.
- [SDR 95ZZZY0723](https://openairdocs.org/sdr/95ZZZY0723), Apr 5, 1995: TRANSDUCER. DEFECTIVE. PRESSURE TRANSDUCER UNIT CAUSES INDICATOR NEEDLE TO FLUCTUATE. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.
- [SDR 95ZZZX2584](https://openairdocs.org/sdr/95ZZZX2584), Mar 28, 1995: INDICATOR. READS HIGH. FUEL QUANTITY GAUGE READS HIGH. COULD NOT CALIBRATE DOWN. REPLACED WITH NEW UNIT. CORRECTED PROBLEM.
- [SDR 95ZZZX5498](https://openairdocs.org/sdr/95ZZZX5498), Mar 24, 1995: BEARING. WORN. NR 3 BEARING, EXCESSIVE ROLLER WEAR. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.
- [SDR 95ZZZX5497](https://openairdocs.org/sdr/95ZZZX5497), Mar 24, 1995: BEARING. PITTED. BEARING OUTER RACE HAS EXCESSIVE PITTING. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.
- [SDR 95ZZZX5311](https://openairdocs.org/sdr/95ZZZX5311), Mar 24, 1995: SEAL. LEAKING. NR 3 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.
- [SDR 95ZZZX5310](https://openairdocs.org/sdr/95ZZZX5310), Mar 24, 1995: SEAL. LEAKING. NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.
- [SDR 95ZZZX5584](https://openairdocs.org/sdr/95ZZZX5584), Mar 20, 1995: GOOSE NECK. CRACKED. GOOSE NECK CRACKED BEYOND SERVICEABLE LIMITS. REPLACED WTIH NEW UNIT(S) CORRECTED PROBLEM.

## STCs that may be installed (OpenAirDocs) (160, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Pilatus PC-12/45)

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA02742NY](https://openairdocs.org/stc/SA02742NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-N-C-F-R(P)/CFR260-65. MT- Propeller Entwicklung GmbH
- [STC SA04763NY](https://openairdocs.org/stc/SA04763NY): Installation of of Gogo Galileo HDX. Pro Star Aviation LLC
- [STC SA03275CH](https://openairdocs.org/stc/SA03275CH): Installation of an antiskid brake system. Lee Air Inc
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA04841NY](https://openairdocs.org/stc/SA04841NY): Installation of replacement LED recognition lights, LED wingtip lights, LED beacon lights, LED taxi lights, and LED landing lights. Whelen Aerospace Technologies
- [STC SA04278NY](https://openairdocs.org/stc/SA04278NY): Installation of the GPS/Iridium Antenna Provisions. SKYTRAC Systems Ltd
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC SA01527CH](https://openairdocs.org/stc/SA01527CH): Installation of a Honeywell KMH 880 Multi-Hazard Awareness System or a Honeywell KTA 870 Traffic Advisory System. Amphenol Cable and Interconnect Technologies Inc
- [STC SA04220NY](https://openairdocs.org/stc/SA04220NY): Installation of Retractable Camera Mount System. Trine Aerospace & Defense
- [STC SA02558SE](https://openairdocs.org/stc/SA02558SE): Installation of a Light Emitting Diode (LED) Landing and Taxi Light. AeroLED's Holdings LLC
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA00028MC](https://openairdocs.org/stc/SA00028MC): Installation of non-essential antenna and radome. Sierra Nevada Company LLC
- [STC SA03316CH](https://openairdocs.org/stc/SA03316CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development Inc
- [STC SA00229MC](https://openairdocs.org/stc/SA00229MC): Installation of Dual Mode Recognition Lights. Sierra Nevada Company LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02266LA](https://openairdocs.org/stc/SA02266LA): Installation of a Pratt and Whitney PT6A-67P. Finnoff Aviation Products LLC
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA00076IB](https://openairdocs.org/stc/SA00076IB): Installation of Photo luminescent Safety Systems. STG AEROSPACE GERMANY GmbH
- [STC SA03097AT](https://openairdocs.org/stc/SA03097AT): Installation of Cabin Interior Light Emitting Diode (LED) Reading and Wash Lights and Air Gaspers. Woven Electronics, LLC
- [STC SA01044DE](https://openairdocs.org/stc/SA01044DE): This STC approves the Finnoff Aviation Products installation of the TB44 advanced lithium-ion battery manufactured by True Blue Power in the make and model listed above (Single Battery Configuration). Finnoff Aviation Products
- [STC SA01376CH](https://openairdocs.org/stc/SA01376CH): Installation of Parker Hannifin Wheel/Brake Assembly P/N 40-424/30-244 (conversion kit no. 199-241). KAMAN Corporation Aircraft Wheel and Brake LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA02254AK](https://openairdocs.org/stc/SA02254AK): Installation of "Single Screen", "2 or 3 Screen", "Dual Screen", or "4 or 6 screen". Genesys Aerosystems Inc
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King)
- [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA04556NY](https://openairdocs.org/stc/SA04556NY): Installation of so-called Seat Slides JG into the cabin. J.G.A
- [STC SA00272LA](https://openairdocs.org/stc/SA00272LA): Installation of a Patient Loading Utility System (PLUS). LifePort LLC
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA02427AK](https://openairdocs.org/stc/SA02427AK): Installation of the Max-Viz® Enhanced Vision System (EVS) Model-1500 on Pilatus PC-12 aircraft equipped with a fixed-mounted or panel-mounted Multi-Function Display (MFD) with the ability to display video imagery. PECO Inc
- [STC SA01116WI-D](https://openairdocs.org/stc/SA01116WI-D): Installation of a Honeywell AM-250 Altimeter. Honeywell International Inc
- [STC SA01253WI-D](https://openairdocs.org/stc/SA01253WI-D): Approved for model PC-12/45, S/N 101 and after, not to exceed S/N 540. Group airworthiness approval for Reduced Vertical Separation Minimum (RVSM). Honeywell International Inc
- [STC SA00886WI-D](https://openairdocs.org/stc/SA00886WI-D): Installation of Honeywell KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS) with optional KMD 550/850 Multi-Function Display. Honeywell International Inc
- [STC SA01524WI-D](https://openairdocs.org/stc/SA01524WI-D): Models PC-12, PC-12/45 and PC-12/47 - Installation of the alternate part number EFS 40/50 SG 465 Symbol Generator. Honeywell International Inc
- [STC SA00393BO](https://openairdocs.org/stc/SA00393BO): Installation of the Pratt & Whitney Engine Services FAST System. Pratt & Whitney Engine Services Inc
- [STC SA01865WI](https://openairdocs.org/stc/SA01865WI): Installation of Generator 2 RCCB Upgrade and/or Dual Battery Cockpit Labeling. Finnoff Aviation Products
- [STC SA01855WI](https://openairdocs.org/stc/SA01855WI): Installation of the Send Solutions Airtext Router in 14 CFR Part 23 Aircraft. 3S Certification LLC
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc

All 160: https://openairdocs.org/aircraft/N911VU/stcs.md

## Related

- Other Pilatus PC-12/45 aircraft: https://openairdocs.org/model/pilatus-pc-12-45/aircraft.md
- The Pratt & Whitney Canada PT6A-67B engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-67b.md

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